Airbus Helicopters H215 vs Leonardo Aw139 vs Leonardo Aw189
The Airbus Helicopters H215 is typically positioned as a heavy, twin‑engine utility helicopter suited to lift- and volume-driven missions (offshore support, SAR, and public services). Compared with the two Leonardos, it generally offers the greatest cabin volume and the highest passenger potential, commonly configured around the high‑teens to low‑20s in an airline-style layout, with range that is competitive but often more mission- and tank‑option dependent. The Leonardo AW139 is a medium, twin‑engine helicopter optimized for speed, flexibility, and high utilization in EMS, corporate/VIP, law enforcement, and short- to mid‑range offshore roles. It usually seats fewer passengers than the H215 and AW189, commonly in the low‑ to mid‑teens, with a practical range suited to regional legs rather than the longest offshore sectors. The Leonardo AW189 sits in the super‑medium class between the AW139 and heavier types like the H215. It generally carries more passengers than the AW139 (often mid‑ to high‑teens) and is designed for longer-range offshore and SAR missions, typically offering greater range and payload capability than the AW139 while remaining smaller than the H215.
| Spec | AIRBUS H215 | AGUSTA / LEONARDO AW139 | AGUSTA / LEONARDO AW189 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 19.07 | $ 11.69 | $ 15.57 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 17 | 21 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Leonardo | Leonardo |
| Aircraft Name | H215 | AW139 | AW189 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 468 | 573 | 651 |
| DOC / nm / Seat | $ 0.91 | $ 0.69 | $ 0.74 |
| Max Cabin Seats | 22 | 15 | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 8903 | 4701 | — |
| Standard Cabin Seats | 19 | 15 | 19 |
| Direct Operating Cost | $ 2,708 | $ 1,929 | $ 2,413 |
| Flight Deck (Base Spec) | EFIS | EFIS | EFIS |
| Max Cruise Speed (ktas) | 142 | 165 | 155 |
| Base Aircraft Price (USD) | $27,500,000 | $15,900,000 | $2,413,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 17 | 21 |
| Max Cabin Seats | 22 | 15 | 19 |
| Standard Cabin Seats | 19 | 15 | 19 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 1A1 | PT6C-67C | CT7-2E1 |
| Fuel Type | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 3000 | 5000 | 4000 |
| Horsepower | 1820 | 1679 | 1983 |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 540 | 414 | — |
| Dimensions | |||
| Length (ft) | 61.4 | 54.7 | 57.8 |
| Overall Height (ft) | 16.2 | 16.4 | 16.6 |
| Rotor Diameter (ft) | 51.2 | 54.7 | 48 |
| Cabin Volume (cu. ft) | 473.9 | 282 | 395 |
| Baggage Volume Ext. (cu. ft) | — | 120 | 85 |